NO863017L - ALUMINUM ALLOY. - Google Patents
ALUMINUM ALLOY.Info
- Publication number
- NO863017L NO863017L NO863017A NO863017A NO863017L NO 863017 L NO863017 L NO 863017L NO 863017 A NO863017 A NO 863017A NO 863017 A NO863017 A NO 863017A NO 863017 L NO863017 L NO 863017L
- Authority
- NO
- Norway
- Prior art keywords
- aluminum
- alloy
- weight
- manganese
- magnesium
- Prior art date
Links
- 229910000838 Al alloy Inorganic materials 0.000 title claims description 8
- 229910045601 alloy Inorganic materials 0.000 claims description 29
- 239000000956 alloy Substances 0.000 claims description 29
- 229910052782 aluminium Inorganic materials 0.000 claims description 18
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 18
- 229910052749 magnesium Inorganic materials 0.000 claims description 13
- 239000011777 magnesium Substances 0.000 claims description 13
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims description 12
- 229910052738 indium Inorganic materials 0.000 claims description 12
- 229910052748 manganese Inorganic materials 0.000 claims description 12
- 239000011572 manganese Substances 0.000 claims description 12
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 claims description 11
- APFVFJFRJDLVQX-UHFFFAOYSA-N indium atom Chemical compound [In] APFVFJFRJDLVQX-UHFFFAOYSA-N 0.000 claims description 11
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 8
- 229910052742 iron Inorganic materials 0.000 claims description 4
- 238000005260 corrosion Methods 0.000 description 15
- 230000007797 corrosion Effects 0.000 description 15
- 239000003792 electrolyte Substances 0.000 description 9
- HEMHJVSKTPXQMS-UHFFFAOYSA-M Sodium hydroxide Chemical compound [OH-].[Na+] HEMHJVSKTPXQMS-UHFFFAOYSA-M 0.000 description 6
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 6
- 239000000243 solution Substances 0.000 description 6
- 229910052718 tin Inorganic materials 0.000 description 6
- 238000005275 alloying Methods 0.000 description 5
- 230000000694 effects Effects 0.000 description 5
- 238000010438 heat treatment Methods 0.000 description 5
- GYHNNYVSQQEPJS-UHFFFAOYSA-N Gallium Chemical compound [Ga] GYHNNYVSQQEPJS-UHFFFAOYSA-N 0.000 description 4
- 238000007792 addition Methods 0.000 description 4
- 229910052733 gallium Inorganic materials 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 239000000203 mixture Substances 0.000 description 4
- 238000001816 cooling Methods 0.000 description 3
- 230000003071 parasitic effect Effects 0.000 description 3
- 229910052710 silicon Inorganic materials 0.000 description 3
- 239000010703 silicon Substances 0.000 description 3
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 2
- TVQLLNFANZSCGY-UHFFFAOYSA-N disodium;dioxido(oxo)tin Chemical compound [Na+].[Na+].[O-][Sn]([O-])=O TVQLLNFANZSCGY-UHFFFAOYSA-N 0.000 description 2
- 239000012535 impurity Substances 0.000 description 2
- 239000003112 inhibitor Substances 0.000 description 2
- 229910002059 quaternary alloy Inorganic materials 0.000 description 2
- 229940079864 sodium stannate Drugs 0.000 description 2
- 229940071182 stannate Drugs 0.000 description 2
- 125000005402 stannate group Chemical group 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 229910052719 titanium Inorganic materials 0.000 description 2
- 239000010936 titanium Substances 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- 239000012670 alkaline solution Substances 0.000 description 1
- 239000004411 aluminium Substances 0.000 description 1
- WNROFYMDJYEPJX-UHFFFAOYSA-K aluminium hydroxide Chemical compound [OH-].[OH-].[OH-].[Al+3] WNROFYMDJYEPJX-UHFFFAOYSA-K 0.000 description 1
- 229910002056 binary alloy Inorganic materials 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 238000005097 cold rolling Methods 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 238000002425 crystallisation Methods 0.000 description 1
- 230000008025 crystallization Effects 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 230000002401 inhibitory effect Effects 0.000 description 1
- 230000005764 inhibitory process Effects 0.000 description 1
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 229910052698 phosphorus Inorganic materials 0.000 description 1
- 239000011574 phosphorus Substances 0.000 description 1
- 238000001556 precipitation Methods 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 230000001172 regenerating effect Effects 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 238000007790 scraping Methods 0.000 description 1
- 239000004334 sorbic acid Substances 0.000 description 1
- 229910002058 ternary alloy Inorganic materials 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 239000011135 tin Substances 0.000 description 1
- 238000013022 venting Methods 0.000 description 1
- 230000004580 weight loss Effects 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M4/00—Electrodes
- H01M4/02—Electrodes composed of, or comprising, active material
- H01M4/36—Selection of substances as active materials, active masses, active liquids
- H01M4/38—Selection of substances as active materials, active masses, active liquids of elements or alloys
- H01M4/46—Alloys based on magnesium or aluminium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/06—Alloys based on aluminium with magnesium as the next major constituent
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/10—Energy storage using batteries
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Electrochemistry (AREA)
- General Chemical & Material Sciences (AREA)
- Primary Cells (AREA)
- Battery Electrode And Active Subsutance (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
Description
Denne oppfinnelse vedrører anoder for elektrokjemiske celler og mer spesielt til en aluminium legering anode som har høy energi og høyt elektrokjemisk potensial i cellene under anvendelse av sterke alkaliske oppløsninger. This invention relates to anodes for electrochemical cells and more particularly to an aluminum alloy anode which has high energy and high electrochemical potential in the cells using strong alkaline solutions.
Grunnkravet til en tilfredstillende anode for elektrokjemiske celler, så som aluminium-luft celler, er enden til å The basic requirement for a satisfactory anode for electrochemical cells, such as aluminium-air cells, is the end to
generere en høy celle spenning mens det oppstår parasittisk korrosjon. Høy spenning er essentielt da det muliggjør ned-settelse av antall celler som er nødvendig for å konstruere et batteri med en gitt spenning. Lav parasittiske korrosjon eller med andre ord høy effektivitet fører til høyere ener-gitetthet, dvs. lavere anode kostnader og viktigere til generate a high cell voltage while parasitic corrosion occurs. High voltage is essential as it enables the reduction of the number of cells necessary to construct a battery with a given voltage. Low parasitic corrosion or in other words high efficiency leads to higher energy density, i.e. lower anode costs and more importantly to
minimering av hydrogengassdannelsen. Hvis denne hydrogen-gass ikke luftes ut og fortynnes tilstrekkelig er det mulig eksplosjons fare. Videre medfører utluftningsoperasjonen selv mulig problemer med avseiling av batteriene for å for-hindre spill. minimization of hydrogen gas formation. If this hydrogen gas is not vented out and diluted sufficiently, there is a possible danger of explosion. Furthermore, the venting operation itself causes possible problems with unsealing the batteries to prevent leaks.
Mye tidligere forskning har basert på tilsetningen av stannat til alkaliske elektrolytter for å kontrollere den parasittiske korrosjon på aluminiumanodene. En foretrukket elektorlytt som har vært anvendt består av 4 molar natrium hydroksyd, 1 molar oppløst aluminium og 0,06 molar natrium stannat (korrosjons hemmer). Likevel foreligger en rekke ulemper ved anvendelsen av en slik elektrolytt nemlig de følgende: 1. Tinn har en tendens til elektorlytten å belegge seg på anoden og derved danne en dendritisk struktur som tilslutt kortslutter cellen. 2. Når tinnetfletterer, avtar dens konsentrasjon i oppløs-ningen med det resultat at den hemmende innflytelse av tin-net tiltagende går tapt; 3. I nærvær av stannat nedsettes veksten av aluminium hydroksyd krystaller og dette resulterer i reduksjon av effektiviteten i enhver regenerativ krystalliserings enhet. Much previous research has relied on the addition of stannate to alkaline electrolytes to control the parasitic corrosion of the aluminum anodes. A preferred electrolyte that has been used consists of 4 molar sodium hydroxide, 1 molar dissolved aluminum and 0.06 molar sodium stannate (corrosion inhibitor). Nevertheless, there are a number of disadvantages with the use of such an electrolyte, namely the following: 1. Tin has a tendency for the electrolyte to deposit on the anode and thereby form a dendritic structure which eventually short-circuits the cell. 2. When the tin braids, its concentration in the solution decreases with the result that the inhibiting influence of the tin mesh is increasingly lost; 3. In the presence of stannate, the growth of aluminum hydroxide crystals is reduced and this results in the reduction of the efficiency of any regenerative crystallization unit.
Mange studier har også vært utført på sammensetningen av anoden. F. eks. beskriver Pryor, et al i US-patent nr. 3.189.486 en anode bestående i det vesentlige av aluminium og tinn, fortrinnsvist med indium. Den fordelaktive effekt av gallium, indium og fosfor på en elektrokjemisk aktivitet er beskrevet i Despic, et al i US-patent nr. 4.288.500. Når tilsatt itl superrent aluminium hever disse elementer i anodiske potensialer. Many studies have also been carried out on the composition of the anode. For example Pryor, et al in US Patent No. 3,189,486 describes an anode consisting essentially of aluminum and tin, preferably with indium. The beneficial effect of gallium, indium and phosphorus on an electrochemical activity is described in Despic, et al in US Patent No. 4,288,500. When added itl superpure aluminium, these elements raise anodic potentials.
Moden, et al i US-patent nr. 4.107.406 beskriver en anode fremstilt av superrent aluminium som inneholder små mengder med magnesium og gallium. Moden, et al in US Patent No. 4,107,406 describes an anode made of superpure aluminum containing small amounts of magnesium and gallium.
Dog utviser ingen av disse ovenfor nevnte legeringer aks-eptabel virkning når anvendt med en sterk alkalisk elektrolytt uten korrosjonshemmer. However, none of these above-mentioned alloys exhibit acceptable performance when used with a strong alkaline electrolyte without a corrosion inhibitor.
I henhold til foreliggende oppfinnelse oppnås en spesiell According to the present invention, a special
fordelaktig balanse med potensial og korrosjonshemming i en alkalisk elektrolytt når anoden fremstilles av en aluminium basert legering med spesielle små tilsetninger av indium og minst enten mangan eller magnesium. Spesielt består legeringen i henhold til oppfinnelsen hovedsaklig av 0,01 til 0,20 vekt-% indium, minst enten 0,01 til 0,25 vekt-% mangan eller 0,01 til 1,5 vekt-% magnesium og resten aluminium, dvs. en aluminium med minst 99,95 % og fortrinnsvist minst 99,99% renhet. En anode fremstilt av legeringen i henhold til foreliggende oppfinnelse har spesielt fordelaktig for anvendelse med en sterk alkalisk elektrolytt, og frembringer en utmerket balanse med potensial og korrosjons resist-ent uten at det er nødvendig å tilsette natrium stannat. advantageous balance with potential and corrosion inhibition in an alkaline electrolyte when the anode is made of an aluminum-based alloy with special small additions of indium and at least either manganese or magnesium. In particular, the alloy according to the invention mainly consists of 0.01 to 0.20 wt% indium, at least either 0.01 to 0.25 wt% manganese or 0.01 to 1.5 wt% magnesium and the rest aluminum, i.e. an aluminum with at least 99.95% and preferably at least 99.99% purity. An anode made from the alloy of the present invention is particularly advantageous for use with a strong alkaline electrolyte, producing an excellent balance of potential and corrosion resistance without the need to add sodium stannate.
Det har vært funnet at nærværet av mangan i legeringen er viktig for å minimere korrosjon under oppladningsbetingel-ser, mens nærværet av magnesium er fordelaktig for å minimere korrosjon under ikke-1adningsbetingelser. I henhold til dette er nærværet av både mangan og magnesium foretrukket . It has been found that the presence of manganese in the alloy is important in minimizing corrosion under charging conditions, while the presence of magnesium is beneficial in minimizing corrosion under non-charging conditions. Accordingly, the presence of both manganese and magnesium is preferred.
Legeringen kan også også tolerere nærværet av jern i mengder opptil ca. 0,03 vekt-% uten at dette fører til sterkt forhøyet korrosjon. Andre komponenter som kan foreligge i legeringen omfatter silikon, tinn, titan og gallium. The alloy can also tolerate the presence of iron in amounts up to approx. 0.03% by weight without this leading to greatly increased corrosion. Other components that may be present in the alloy include silicon, tin, titanium and gallium.
En foretrukket legering inneholder 0,05 itl 1,0 vekt-% magnesium, 0,02 til 0,15 vekt-% indium, 0,02 til 0,2 vekt-%-mangan og resten er superren aluminium. Denne legering kan også inneholde andre mindre komponenter så som opptil 0,005 vekt-% silikon, opptil 0,005 vekt-% tinn, opptil 0,005 vekt-% titan og 0,005 vekt-% gallium. Disse komponenter samt jern kan enten allerede foreligge i det superrene grunnaluminiumet eller innføres som urenheter med de legerende tilsetninger. A preferred alloy contains 0.05 to 1.0 wt% magnesium, 0.02 to 0.15 wt% indium, 0.02 to 0.2 wt% manganese and the balance is super pure aluminum. This alloy may also contain other minor components such as up to 0.005 wt% silicon, up to 0.005 wt% tin, up to 0.005 wt% titanium and 0.005 wt% gallium. These components and iron can either already be present in the super-pure basic aluminum or introduced as impurities with the alloying additions.
Legeringssammensetningen kan bearbeides ved en rekke kon-vensjonelle støpemetoder, hvilke omfatter permanente labor-atorie støpeformer, tovalse eller to belte støpere og de vanlige direkte avkjølingsmetoder. Et viktig trekk ved oppfinnelsen er å sikre at et minimumsnivå av de legerende be-standdeler er i oppløsning til i det minste en vesentlig grad. I henhold til dette kan fremgangsmåtene omfatte en varmebehandling av oppløsningen enten på barren eller det mellomliggende tykkelses trinnet. Dette kan oppnås ved varmebehandling i 8 timer ved 600°C påfulgt av en vann-avkjøling. Flaten kan enten bearbeides varmt eller kaldt, men det må utvises forsiktighet ved varmbearbeiding eller mellomliggende varmebehandling grunnet muligheten for ut-felling av legerende elementer ved forlenget utsettelse for temperaturer under oppløsningstemperaturen. Nærværet av ut-feldte legerende elementer i mikrostrukturen kan nedsette effektiviteten til anoden. The alloy composition can be processed by a number of conventional casting methods, which include permanent laboratory molds, two-roll or two-belt casters and the usual direct cooling methods. An important feature of the invention is to ensure that a minimum level of the alloying constituents is in solution to at least a significant extent. According to this, the methods can include a heat treatment of the solution either on the ingot or the intermediate thickness step. This can be achieved by heat treatment for 8 hours at 600°C followed by a water cooling. The surface can either be processed hot or cold, but care must be taken during hot processing or intermediate heat treatment due to the possibility of precipitation of alloying elements during prolonged exposure to temperatures below the solution temperature. The presence of precipitated alloying elements in the microstructure can reduce the efficiency of the anode.
Visse foretrukne utførelsesformer av oppfinnelsen skal nå illustreres ved de følgende eksempler. Certain preferred embodiments of the invention will now be illustrated by the following examples.
EKSEMPEL 1EXAMPLE 1
En rekke legeringer ble fremstilt utgående fra superrent aluminium (minst 99,990% renhet) og forskjellige legerende elementer ble tilsatt som antydet i tabell 1. Legeringene 1 til 8 ble støpt til barrer med tykkelse på 19 mm og barrene ble skrapt for å fjerne omtrent 0,15 mm fra hver hoved- ' flate. Disse artikler ble utsatt for oppløsnings varmebehandling i 8 timer ved 600°C og påfølgende en vannavkjøl-ing, ble kaldrullet for å danne plater med tykkelse på 3,2 mm. Legeringen 9-14 ble bearbeidet på samme måte med det tillegg av et ytterligere kaldrullingstrinn til 14 mm påfulgt av skraping men før oppløsnings varmebehandlingen. Denne tilleggs operasjonen hadde ingen målbar effekt på egenskapene oppført i tabell 1. A series of alloys were prepared starting from superpure aluminum (at least 99.990% purity) and various alloying elements were added as indicated in Table 1. Alloys 1 to 8 were cast into 19 mm thick ingots and the ingots were scraped to remove approximately 0, 15 mm from each main surface. These articles were subjected to solution heat treatment for 8 hours at 600°C and following a water cooling, were cold rolled to form plates with a thickness of 3.2 mm. Alloy 9-14 was processed in the same way with the addition of a further cold rolling step to 14 mm followed by scraping but before the solution heat treatment. This additional operation had no measurable effect on the properties listed in Table 1.
Legeringsplåtene dannet slik ble utprøvd som anoder og deres egenskaper for å generere celle spenninger på åpen strømkrets og med ytre strømstyrker på 200 og 600 mA/cm<2>(EOC, E200, E600) ved 60°C i 4 molar NaOH. Korrosjonstrøm ble målt som vekttap ved åpen strømkrets og med ytre strøm-styrker på 200 og 600 mA/cm<2>(henholdsvis ICOC, IC200, IC600) ble også bestemt. The alloy plates thus formed were tested as anodes and their properties for generating cell voltages on open circuit and with external currents of 200 and 600 mA/cm<2> (EOC, E200, E600) at 60°C in 4 molar NaOH. Corrosion current was measured as weight loss at open circuit and with external current strengths of 200 and 600 mA/cm<2> (respectively ICOC, IC200, IC600) were also determined.
Legeringsammensetningene og de elektrolyttiske resultater er oppført i tabell 1 nedenfor. Fra tabellen ovenfor er det klart at binære legeringer var helt utilstrekkelige. Fra tabell 1 kan det også sees på grunnlag av de høye potensialer og lave korrosjonsstrøm-styrker at ternære og kvartnære legeringer som inneholdt Mn, Mg og In frembringer de mest nyttige kompromiss av alle legeringene som ble utprøvd. Det er også klart at oppbygg-ing av oppløst legering i elektrolytten, f.eks. som repre-sentert ved utprøving av legering 8 i elektrolytten med 27 g/l av oppløst legering ikke påvirker virkningen negativt. The alloy compositions and electrolytic results are listed in Table 1 below. From the above table it is clear that binary alloys were completely inadequate. From Table 1 it can also be seen on the basis of the high potentials and low corrosion current strengths that ternary and quaternary alloys containing Mn, Mg and In produce the most useful compromises of all the alloys tested. It is also clear that build-up of dissolved alloy in the electrolyte, e.g. as represented by testing alloy 8 in the electrolyte with 27 g/l of dissolved alloy does not affect the effect negatively.
EKSEMPEL 2EXAMPLE 2
For å vise effekten av mangan på korrosjonshastigheten under ladning av legeringen i henhold til oppfinnelsen ble det fremstilt 8 forkjellige legeringer utgående fra superren aluminium (minst 99,990% renhet). Disse ble støpt inne-holdene to forskjellige konsentrasjoner av magnesium og indium og med og uten mangan, under anvendelse av samme fremgangsmåte som anvendt for legeringene 1-8 av eksempel 1. Korrosjonen ved ladning på 200 mA/cm<2>ble målt som i eksempel 1, alle mål ble tatt tre ganger og middelverdien oppført. Resultatene er vist i tabell 2 nedefor: In order to show the effect of manganese on the corrosion rate during charging of the alloy according to the invention, 8 different alloys were produced starting from superpure aluminum (at least 99.990% purity). These were cast containing two different concentrations of magnesium and indium and with and without manganese, using the same method as used for the alloys 1-8 of example 1. The corrosion at a charge of 200 mA/cm<2> was measured as in example 1, all measurements were taken three times and the mean value listed. The results are shown in table 2 below:
Det vil sees fra resultatene ovenfor at de kvartanære legeringer har de laveste korrosjonshastigheter. It will be seen from the above results that the quaternary alloys have the lowest corrosion rates.
EKSEMPEL 3EXAMPLE 3
For å bestemme effektene til forurensninger på legeringer i henhold til oppfinnelsen ble en rekke aluminiumslegeringér støpt fra superrent aluminium som inneholdt forskjellige konsentrasjoner av jern og silikon, sammen med relativt lave konsentrasjoner av magnesium, mangan og indium. En høy renhets grunnsubstans og en kommersiell ren grunnsubstans ble også anvendt. Fremgangsmåten anvendt var den samme som den for legeringene 1-8 i eksempel 1. To determine the effects of impurities on alloys according to the invention, a series of aluminum alloys were cast from superpure aluminum containing various concentrations of iron and silicon, together with relatively low concentrations of magnesium, manganese and indium. A high purity parent substance and a commercial pure parent substance were also used. The procedure used was the same as that for alloys 1-8 in Example 1.
Legerings sammensetningene og resultatene, målt som i eksempel 1 er vist i tabell 3 nedenfor: The alloy compositions and results, measured as in Example 1 are shown in Table 3 below:
Claims (9)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CA487563 | 1985-07-26 | ||
CA510488 | 1986-05-30 |
Publications (2)
Publication Number | Publication Date |
---|---|
NO863017D0 NO863017D0 (en) | 1986-07-25 |
NO863017L true NO863017L (en) | 1987-01-27 |
Family
ID=25670753
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
NO863017A NO863017L (en) | 1985-07-26 | 1986-07-25 | ALUMINUM ALLOY. |
Country Status (6)
Country | Link |
---|---|
US (1) | US4751086A (en) |
EP (1) | EP0209402A1 (en) |
JP (1) | JPS6274041A (en) |
AU (1) | AU592106B2 (en) |
IN (1) | IN167995B (en) |
NO (1) | NO863017L (en) |
Families Citing this family (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4865651A (en) * | 1987-07-24 | 1989-09-12 | Aluminum Company Of America | Method of making an aluminum base alloy anode |
US4808498A (en) * | 1987-12-21 | 1989-02-28 | Aluminum Company Of America | Aluminum alloy and associated anode |
GB8801663D0 (en) * | 1988-01-26 | 1988-02-24 | Alcan Int Ltd | Aluminium batteries |
US4950560A (en) * | 1988-08-01 | 1990-08-21 | Aluminum Company Of America | Aluminum alloy and associated anode and battery |
NZ230197A (en) * | 1988-08-09 | 1990-11-27 | Alcan Int Ltd | Aluminium battery with an aluminium alloy anode and containing tin in the anode and/or the electrolyte |
US4942100A (en) * | 1988-08-09 | 1990-07-17 | Alcan International Limited | Aluminium batteries |
DE4023951C2 (en) * | 1990-07-27 | 1994-08-04 | Dieter Dr Remppel | Process for dynamically changing the electrochemical behavior of metallic materials |
US5413881A (en) * | 1993-01-04 | 1995-05-09 | Clark University | Aluminum and sulfur electrochemical batteries and cells |
JPH07462U (en) * | 1993-04-19 | 1995-01-06 | 昇 羽賀 | Code for pachinko |
JP2907718B2 (en) * | 1993-12-29 | 1999-06-21 | 昭和アルミニウム株式会社 | Etching method of aluminum foil for electrolytic capacitor electrode |
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US2464821A (en) * | 1942-08-03 | 1949-03-22 | Indium Corp America | Method of preparing a surface for soldering by coating with indium |
FR89561E (en) * | 1963-01-14 | 1900-01-01 | ||
US3379636A (en) * | 1964-07-23 | 1968-04-23 | Dow Chemical Co | Indium-gallium-aluminum alloys and galvanic anodes made therefrom |
US3830635A (en) * | 1971-05-26 | 1974-08-20 | Southwire Co | Aluminum nickel alloy electrical conductor and method for making same |
YU40575A (en) * | 1975-02-20 | 1982-02-25 | Inst Tehnickih Nauka Sanu | Alloy of aluminium with indium or gallium or thallium |
JPS572855A (en) * | 1980-06-06 | 1982-01-08 | Showa Alum Corp | Cathodically protecting aluminum alloy for vacuum brazing |
JPS5712754A (en) * | 1980-06-26 | 1982-01-22 | Misawa Homes Co | Arrangement of roof plywood |
JPS6086760A (en) * | 1983-10-19 | 1985-05-16 | Matsushita Electric Ind Co Ltd | Nonaqueous electrolyte secondary battery |
-
1986
- 1986-07-14 IN IN623/DEL/86A patent/IN167995B/en unknown
- 1986-07-22 US US06/888,779 patent/US4751086A/en not_active Expired - Fee Related
- 1986-07-25 EP EP86305761A patent/EP0209402A1/en not_active Withdrawn
- 1986-07-25 AU AU60554/86A patent/AU592106B2/en not_active Ceased
- 1986-07-25 NO NO863017A patent/NO863017L/en unknown
- 1986-07-25 JP JP61175457A patent/JPS6274041A/en active Pending
Also Published As
Publication number | Publication date |
---|---|
AU6055486A (en) | 1987-01-29 |
NO863017D0 (en) | 1986-07-25 |
JPS6274041A (en) | 1987-04-04 |
US4751086A (en) | 1988-06-14 |
EP0209402A1 (en) | 1987-01-21 |
AU592106B2 (en) | 1990-01-04 |
IN167995B (en) | 1991-01-19 |
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